CHI03LA043

NTSB accident investigation · Piper PA-28-235 · Carleton, MI · December 22, 2002

Accident · No injuriesLimited investigationFinal report
Date
December 22, 2002, 17:00 local (22:00 UTC)
Place
Carleton, MI
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N8555WPiper PA-28-235
Weather
Visual (VMC) · Day
Status
Completed · report June 25, 2003
Report
Approved by Office Director
Parties
FAA - Detroit FSDO
FAA report
20021222035669A
Case key
56242

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

The #2 cylinder exhaust valve failed due to undetermined reasons. A factor associated with the accident was the soft terrain encountered during the forced landing.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Loss of engine power(partial) - mech failure/malfCruise - normal
Engine assembly,valve,exhaust - failure,totalCause
Forced landingEmergency descent/landing
Nose gear collapsedLanding - roll
Terrain condition - softFactor
Landing gear,nose gear assembly - overload

Analysis

The nose gear collapsed during an off airport forced landing following a loss of engine power. The pilot reported that while en route to his destination, the engine power dropped to 1,300 rpm. He stated he applied carburetor heat, turned on the auxiliary fuel pump, and switched fuel tanks to no avail. The pilot reported that the passenger checked the engine instruments and all indications were normal. The pilot contacted the Willow Run Air Traffic Control Tower and informed them of the situation, stating that he was going to land at their airport. After turning toward the airport, the pilot determined he was not going be able to reach the airport, so he pilot selected a plowed field in which to land. The nose gear collapsed during the landing and the airplane came to rest on the engine cowling and main landing gear. Examination of the engine revealed the #2 cylinder exhaust valve was broken off and a piece of the #2 cylinder was missing. Portions of the exhaust valve and valve stem were recovered from the engine. Visual examination revealed the fractured surfaces were deformed and obscured by impact damage to such a degree that the failure mode could not be determined.

Factual narrative

On December 22, 2002, at 1700 eastern standard time, a Piper PA-28-235, N8555W, operated by a commercial pilot, experienced a nose gear collapse during an off airport forced landing following a loss of engine power. The pilot and passenger were not injured. The airplane received substantial damage. The 14 CFR Part 91 personal flight was operating in visual meteorological conditions without a flight plan. The last leg of the flight originated at Pontiac, Michigan, at 1615.

The pilot reported that while en route to his destination, the engine power dropped to 1,300 rpm. He stated he applied carburetor heat, turned on the auxiliary fuel pump, and switched fuel tanks to no avail. The pilot reported that the passenger checked the engine instruments and all indications were normal. The pilot contacted the Willow Run Air Traffic Control Tower and informed them of the situation, stating that he was going to land at their airport. After turning toward the airport, the pilot determined he was not going be able to reach the airport, so he pilot selected a plowed field in which to land. The nose gear collapsed during the landing and the airplane came to rest on the engine cowling and main landing gear.

The airplane's engine was examined by inspectors from the Federal Aviation Administration Detroit, Michigan, Flight Standards District Office. The inspectors reported that the number 2 cylinder exhaust valve was broken off and a piece of the number 2 cylinder was missing. Portions of the exhaust valve and valve stem were recovered from the engine. Visual examination revealed the fractured surfaces were deformed and obscured by impact damage to such a degree that the failure mode could not be determined.

Aircraft

Registration
N8555W
Reported as
Piper PA-28-235
Category
Airplane
Serial number
28-10069
Engine
Lycoming O-540-B4B5, 235 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Kyle D. Crossman
Airworthiness certificate
Standard, Normal
Last inspection
Annual · February 12, 2002
Departed
PTK · Pontiac, MI
Destination
TFF · Monroe, MI
Airport
YIP · Willow Run

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
34
Injuries
None
Certificate
Commercial
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--w/ waivers/lim
Last flight review
August 15, 2002
Seat
Left
Flight hours
2,085 total · 40 in this make and model · 2,020 as pilot in command · 45 in the last 90 days · 10 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
270° at 20 knots, gusting 26
Visibility
10 statute miles
Lowest ceiling
2,400 ft overcast
Temperature
30 °F, dew point 21 °F
Altimeter
29.80 inHg
Observed at
YIP, 18 nm away

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.

Other investigations on N8555W · 1

Matched to the same aircraft by N-number and date.